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The Modular Wearable Computer (MOWC) is a rugged, lightweight, modular system designed to provide monitoring, command & control, and system status for three separate small unit remote scouting system technologies. The MOWC provides a common control system for the Dragon Eye Unmanned Aerial Vehicle, Dragon Runner Unmanned Ground Vehicle, and Small Unit Sensor System (SUSS) Unattended Ground Sensor.
Description:
A complete MOWC system consists of one CPU, one battery back, one Heads Up Display, and one interface hub. The interface hub features a plug and play display /controller that allows the operator to select and fully control any of the three unmanned sensors from the common control platform. The MOWC system weighs less then 6 lbs.
Product Availability: The MOWC is currently in testing with the USMC. Prototype systems are available through Icuiti for test and evaluation. Custom Interfaces can also be developed for your application
Specifications
Features:
- Low power, high performance
- Small, light weight, rugged design
- Removable hard drive
- 802.11b/g wireless connectivity
- Modular I/O design
Key Applications:
- UAV & UGV Ground Control Station
- Embedded communications
- Body worn, test measurement, maintenance, and communications
- Surveying
- Aviation telemetry
- Situational awareness
Processor
- Intel® Pentium® M 738 processor at 1.4GHz
- System bus: 400MHz
- Intel® 855GME chipset
OS Support
- Windows®2000 Professional/XP Pro
Chassis Construction
- A solid, conductive cooled, rugged cast magnesium aluminum alloy construction protects internal subsystems from shock and vibration
RAM/Cache
- 512MB DDR 333MHz DRAM (PC2700), upgradeable to 1GB
- 64MB Video DRAM
- Standard 2MB L2 cache
Removable Ruggedized 2.5-inch Hard Drive
- 40GB ATA/100 removable hard drive module (standard)
- 60 and 80GB ATA/100 removable hard drive module (optional)
- Heated hard drive upgrade for expanded operating temperature specification
Integrated Wireless LAN
- Integrated Intel® Centrino® Wireless Pro 2200 802.11b/g
- Integrated antenna
- Software controlled radio off/on via OS
Power and Power Management System
- ACPI Compliance, (Standby, Suspend, and Hibernate (S1,S3,S5)
- Graceful shutdown and inactivity timers
- 'Auto on' vehicle key signal on docking connector for remote power on and graceful power down
Environmental
Operating Temperature
- -15 ° to 60 °C (5 ° to 140 °F)
Non-operating Temperature
- -25 ° to 60 °C (-13 ° to 140 °F)
Operating Humidity
- 10 to 90% relative humidity, non-condensing
Non-operating Humidity
- Mil-Std-810F, Method 507.4
- 5 to 95% relative humidity, non-condensing
Water, Dust, Salt Fog
- Rain and blowing rain: Mil-Std 810F, Method 506.4, Procedure I
- Sand and dust: Mil-Std 810F, Method 510.4, Procedure I, II, and III
- Salt fog: Mil-Std 810F, Method 509.4
Non-operating Temperature Option (for ECM only)
- -30 ° to 70 °C (-22 ° to 158 °F)
Extended Temperature Option - Operating (for ECM only)
- -40 ° to 60 °C (-40 ° to 140 °F)*
Extended Temperature Option - Cold Start (for ECM only)
- -25 ° to 60 °C (-13 ° to 140 °F)*
*Power applied to unit at all times
Shock
- Functional: Mil-Std 810F, Method 516.5, Procedure I
- (Operating) 40g at 45Hz - 200Hz; 18 drops
- Crash Hazard: Mil-Std 810F, Method 516.5, Procedure IV
- (Non-Operational) 75g at 80Hz - 2000Hz; 12 drops
Vibration
- Mil-Std 810F, Method 514.4, Procedure 1, Cat. 20, Table 514.5C-VII, Figure
- 514.5C (composite wheeled vehicle)
Hz Power Spectral Density (g2/Hz)
- 10 0.015
- 40 0.015
- 50 0.00015
- Overall acceleration: 1.04g
- Duration: 1hr in each of three mutually perpendicular axes
Operating Altitude
- -300 to 3000-meters (-984 to 9842-feet)
Non-operating Altitude
- -400 to 15,000-meters (-1312 to 49,212-feet)
EMI/EMC & Safety
- FCC Class A, CE Class A, ETL, cETL
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